Unified application of vapor screen flow visualization and pressure sensitive paint measurement techniques to vortex- and shock wave-dominated flow fields /

Bibliographic Details

Main Author:	Erickson, Gary E.
Corporate Author:	Langley Research Center
Format:	Government Document eBook
Language:	English
Published:	Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2010]
Series:	NASA technical memorandum ; 216197.
Subjects:	Aerodynamic configurations. Pressure sensitive paints. Flow visualization. Shock waves. Static pressure. Leading edges. Angle of attack.
Online Access:	https://purl.fdlp.gov/GPO/gpo865